N8691A
Service difficulty reports · 85
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N8691A' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N8691A' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA2026100510312Assist Handle · looseL2 DOOR ASSIST HANDLE NEEDS TO BE SECURED. SECURED THE L2 DOOR ASSIST HANDLE IAW AMM 52-13-31-400-802, SUBTASK 52-13-31-020-008.SDR SWAA2026090818561Barrier · dischargedREAR MEGAPHONE BATTERY DEAD. R & R THE MEGAPHONE IAW AMM 25-64-00. OPS CK GOOD. NEXT INSPECTION DUE 09/2027.SDR SWAA2026082463083Flashlight · no testFA REPORTS FWD FLASHLIGHTS WILL NOT TEST. RESEATED AND RESEALED FWD GALLEY FLASHLIGHTS IAW AMM 25-64-00.SDR SWAA2026062212758Light · brokenRIGHT AFT EXIT ROW LIGHT BROKEN. REPLACED LIGHT ASSY IAW AMM 33-51-01.SDR SWAA2026021169175Flashlight · not seatedAFT GALLEY CAPTAINS SIDE FLASHLIGHT WILL NOT TEST. FOUND AFT GALLEY FLASHLIGHT NOT SEATED CORRECTLY. SEATED THE FLASHLIGHT IAW AMM 25-64-00 OPS CHECKED GOOD.SDR SWAA2026012663398Cover · detachedAISLE CEILING EXIT SIGN COVER BETWEEN OVERWING EXIT ROWS, DETACHED. INSTALLED THE COVER IAW AMM 33-51-01.SDR SWAA2025122955411Lens · detachedEMER EXIT SIGN ROW 15 CENTER AISLE FELL OFF. SECURED OVERHEAD EMERGENCY EXIT LENS COVER PER AMM SIP.SDR SWAA2025112538731Condenser · poppedAPPROX 1000 AGL HEARD LOUD POPPING SOUND. LOUD AIR RUSHING SOUND THAT MADE IT DIFFICULT TO HEAR IN COCKPIT. FAS HEARD SAME LOUD NOISE AND RUSHING AIR NOISE. MIXED WATER AND ICE CRYSTALS AND UNCOMMANDED TEMP CHANGES. NO PRESS CHANGES AND DUCT PRESSURE REMAINED SDR SWAA2025062082940Flashlight · inoperativeAFT FA JUMPSEAT CAPTS SIDE 1 FLASHLIGHT INOP.SDR SWAA2025061681117Light · inoperativeLIGHT ABOVE AFT RIGHT OVERWING EMERGENCY EXIT IS FLASHING ON AND OFF.<[01] EMERGENCY LIGHTS UNAFFECTED BY LIGHT STRIP PER AMM 33-51-00. OK TO CONTINUE PER MEL 33-2-04; SP-1B; AUTH: 260977;[02] OPERATIONAL CHECK OF AFT RH OVERWING EXIT LIGHT GOOD PER AMM 33-20-SDR SWAA2025051968392Lens · brokenAFT OVERHEAD COVE PANEL EMERGENCY EXIT LIGHT LENSE IS BROKEN<[01] REMOVED AND INSTALLED NEW AFT OVERHEAD COVE PANEL EMERGENCY EXIT LIGHT ASSEMBLY PER AMM 33-51-03. OPS CHECK GOOD.;[02] INSPECTED AS REQUIRED; CORRECTIVE ACTION #1SDR SWAA2025051965152Slide · looseFWD ENTRY DOOR SLIDE FWD ATTACH SCREW LOOSE.<[01] SECURED SCREW PER SOPM 20-50-01;[02] C/W INSPECTIONSDR SWAA2025051965155Floorbeam · crackedCABIN FLOOR INTERCOSTAL STA-540 BL-0 TO RBL-24 CRACKED AT RBL-1 (MARKED)<[01] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02.;[02] INSPECTION COMPLETED FOR WORK ACCOMPLISHED; REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02.;[03] INSPECTION COMPLETED FOR WSDR SWAA2025051965009Attach Angle · crackedBS 663 VAPOR BARRIER ATTACH ANGLE CRACKED AT APPROXIMATELY RBL 9.<[01] REMOVED FASTENERS IN FUEL TANK ONLY OF 663 VAPOR BARRIER ANGLE ON R/H SIDE PER SRM 51-40-02;[02] CUT AND REMOVED VAPOR BARRIER ATTACH ANGLE ON STA. 663 FROM APPROXIMATELY RBL 6? TO RBL 17? SDR SWAA2025051965008Attach Angle · crackedBS 663 VAPOR BARRIER ATTACH ANGLE CRACKED AT APPROXIMATELY LBL 9.<[01] REMOVED FASTENERS IN FUEL TANK ONLY OF VAPOR BARRIER ANGLE ON L/H SIDE PER SRM 51-40-02;[02] CUT AND REMOVED VAPOR BARRIER ATTACH ANGLE ON STA. 663 FROM APPROXIMATELY LBL 6? TO LBL 17? PER SDR SWAA2025032107855Megaphone · inoperativeFWD MEGAPHONE INOP <[01] R&R FWD MEGAPHONE IAW AMM 25-64-00.SDR SWAA2024082026407Overheat Loop · faultyWING BODY OVERHEAT LEFT SIDE; EXTINGUISHED 7 OR 8 MINUTES AFTER COMPLETING QRH PROCEDURES<[01] REF FIM 26-18 TASK 801 AND 802. PERFORMED BITE. FAULT 14 DISPLAYED. INSPECTED APPLICABLE DUCTS FOR LEAKS; NONE NOTED. OK TO CONTINUE ON MEL 26-12-01 SP 1 AUTH #20967SDR SWAA2024081926412Flashlight · inoperative2 AFT GALLEY FLASHLIGHTS INOP<[01] REMOVED AND REPLACED FLASHLIGHTS PER 25-64-00 AMM AND CMM 25-60-02. NOTE: NEW EXPIRATION DATE IS 08-2029.SDR SWAA2024080722705Lamp · missingOVERWING EXIT SIGN AT ROW 14 CA SIDE MISSING (AT BOTTOM)<[01] R&R XIT SIGN LAMP PER AMM 33-51-01. OPS CHECK GOODSDR SWAA2024071613064Megaphone · missingAFT GALLEY BULLHORN MISSING VOLUME KNOB<[01] R AND R AFT MEGAPHONE IAW AMM 25-64-00 OPS CK GOODSDR SWAA2024052186687Battery Pack · inoperativeWHILE PERFORMING EMERGENCY LIGHT TEST IAW SWA AMM 33-51-00-720-801 FOUND AISLE LIGHTS IN AFT CABIN INOP<[01] REMOVED AND REPLACED 2 EA AFT CABIN EMERGENCY BATTERY PACKS (OVER L2 AND R2) AND OPS CHECK GOOD IAW SWA B737-800 AMM 33-51-06-960-805.;[02] REMOVED ANDSDR SWAA2024052185205Battery Pack · inoperativeWHILE PERFORMING TEST IAW SWA AMM 33-51-00-720-801; FOUND AISLE LIGHTS AT R/H STA 500 TO STA 589 INOP<[01] REMOVED; REPLACED AND PERFORMED A GOOD CHECK OF THE EMERGENCY AISLE LIGHTS AT R/H STA 500 TO STA 589 IAW SWA AMM 33-51-06.;[02] 02 - INSPECTED PER [AMM 3SDR SWAA2024052183373Battery Pack · failedEMERGENCY BATTERY PACK AT L/H SEAT 20ABC WILL NOT CHARGE<[01] 01 - REMOVED AND REPLACED PER B737 AMM33-51-960-805. OPS CHECK GOOD IAW B737 AMM 33-51-06-960-805;[02] - REMOVED AND REPLACED PER B737 AMM33-51-06-960-805. OPS CHECK GOOD IAW B737 AMM 33-51-06-960-8SDR SWAA2024052182024Strap · crackedAFT CARGO 727 BHD STRAP 144A2617-5 IS CRACKED<[01] REMOVED AND REPLACED AFT CARGO 727 BHD STRAP 144A2617-5 PER BOEING DWG 144A2600 REV-A AND B737-800 SRM 51-40-02.;[02] VERIFIED REMOVAL AND REPLACEMENT OF R/H STRAP AT STA. 727 BHD144A2617-5 PER BOEING DWG 144ASDR SWAA2024052181520Stiffener · crackedAFT FLOOR PANEL 140AF STIFFENER PLATE 453A2611-12 CRACKED IN 2 PLACES<[01] REMOVED AND REPLACED AFT FLOOR PANEL 140AF STIFFENER PLATE 453A2611-12; PO #: 1089820.1 PER B737-800 SRM 51-40-02.;[02] VERIFIED REMOVAL AND REPLACEMENT OF AFT FLOOR PANEL 140AF STIFFENSDR SWAA2024052181773Stringer Clip · crackedFWD PIT R/H SIDE; CLIP CRACKED AT AFT SIDE OF BS 500H APPROX. STRINGER S-26R.<[01] REMOVED AND REPLACED FWD PIT R/H SIDE; CLIP AT AFT SIDE OF BS 500H; S26R PER BAC DWG 143A7505 REV. B AND B737-800 SRM 51-40-02. PO#: 1087455.1;[02] VERIFIED REMOVAL AND REPLACEMSDR SWAA2024052181763Stringer Clip · crackedFWD PIT R/H SIDE; CLIP CRACKED AT FWD SIDE OF BS 500H APPROX. STRINGER S-26R.<[01] REMOVED AND REPLACED FWD PIT R/H SIDE; CLIP AT FWD SIDE OF BS 500H; S-26R IAW BAC DWG 143A7505 REV. B AND B737-800 SRM 51-40-02. PO# 1087457.1;[02] VERIFIED REMOVAL AND REPLACEMSDR SWAA2024052181765Stringer Clip · crackedFWD PIT L/H SIDE; CLIP CRACKED AT FWD SIDE OF BS 500H APPROX. STRINGER S-26L.<[01] REMOVED AND REPLACED FWD PIT L/H SIDE; CLIP AT FWD SIDE OF BS 500H APPROX. STRINGER S-26L PER BOEING DWG 143A7505 REV-B AND B737-800 SRM 51-40-02.;[02] VERIFIED REMOVAL AND REPLSDR SWAA2024052181766Stringer Clip · crackedFWD PIT R/H SIDE; STRINGER CLIP CRACKED AT FWD SIDE OF BS 500I APPROX. STRINGER S-26R.<[01] REMOVED AND REPLACED STRINGER CLIP PN: 143A1010-48 PO# 1090043.1 IAW B737-800 SRM 51-40-02 & BAC DWG# 143A1234 REV. A.;[02] VERIFIED REMOVAL AND REPLACEMENT OF STRINGERSDR SWAA2024052182017Scuff Plate · crackedAFT CARGO DOOR AFT CORNER SCUFF PLATE IS CRACKED * PARTS RACK ITEM *<[01] REPAIRED AFT CARGO DOOR AFT CORNER SCUFF PLATE PER B737-800 SRM 53-60-15-2R-1.;[02] VERIFIED REPAIR AFT CARGO DOOR A CORNER SCUFF PLATE PER B737-800 SRM 53-60-15-2R-1.SDR SWAA2024052182010Floorbeam · crackedMAIN CABIN CRACK FOUND ON PANEL BREAK UNDER PANEL 231XF DOT L625<[01] REPLACED LH PLATE UNDER FLOOR PANEL 231 UF AND 231XF IAW B37-800 SRM 51-40-02-0G-0 AND BAC DWG 143A5240 REV: - & B.;[02] REPLACED LH PLATE UNDER FLOOR PANEL 231 UF AND 231XF IAW B37-800 SRM SDR SWAA2024052182161Rib · wornRIGHT WING TIP AREA; WING RIB 27( AT WBL 658.17) HAS 3 EACH WEAR MARKS AT O/B SURFACE.<SDR SWAA2024052181769Floor Support · corrodedAFT CABIN WET AREA INTERCOSTAL STA.927-947 LBL52 HAS CORROSION AT STA.947<[01] REMOVED AND REPLACED INTERCOSTAL PN 147A5690-3 IAW B737-800 SRM 51-40-02 AND BAC DWG 147A5690;[02] VERIFIED REMOVED AND REPLACED INTERCOSTAL PN 147A5690-3 IAW B737-800 SRM 51-40-02 SDR SWAA2024052182019Skin · corrodedL/H WINGLET TIP HAS CORROSION AT THE TOP.<[01] REMOVED DAMAGE ON L/H WINGLET TIP IAW B737-800 SRM 57-30-01 REPAIR 6;[02] REMOVED DAMAGE ON L/H WINGLET TIP IAW B737-800 SRM 57-30-01 REPAIR 6SDR SWAA2024052182018Strake · corrodedL/H WINGLET AREA; STRAKE HAS CORROSION AT THE TIP AREA.<[01] REMOVED CORROSION FROM AREA IAW B737-800 SRM 57-31-01. ORIGINAL THICKNESS IS .050'. REMOVED .039' OF MATERIAL. REMAINING THICKNESS IS .011'. FOUND TO BE OUT OF LIMITS. TOOL# T8224M CAL DUE: 07/NOV/24SDR SWAA2024052181368Web · crackedAFT WET AREA AFT OF L2 DOOR AT 986 EVIDENCE OF CRACK FOUND ON WEB STRUCTURE DOT L633<[01] PERFORMED SURFACE HFEC ON BLEND AREA IAW B737 NDTM 51-00-00 PROC 23. USING T8257K CAL 28SEP24. NO CRACKS NOTED. WEB REMOVED AND REPLACED ON FAULT TTG8Q00T35FB;[02] PERFORSDR SWAA2024052181517Seal · crackedL/H HORIZONTAL L/E AREA; UPPER SLIDING SEAL CRACKED AT THE LOWER AFT CORNER.<[01] REMOVED AND REPLACED LH UPPER SLIDE SEAL IAW B737-800 AMM 53-31-31-400-802.;[02] TOOL NUMBER T8352R CAL DUE DATE 18/JUL/2024.;[03] VERIFIED REMOVAL AND INSTALLATION OF L/H UPPER SDR SWAA2024052181510Seal · crackedR/H HORIZONTAL L/E AREA; UPPER SLIDING SEAL CRACKED AT THE LOWER AFT CORNER.<[01] REPLACED RH UPPER SLIDE SEAL IAND INSTALLED IAW B737-800 AMM 53-31-31-400-802; B737-800 SRM 51-40-02-0G-0.;[02] VERIFIED REMOVAL AND INSTALLATION OF R/H UPPER SLIDE SEAL IAW B737SDR SWAA2024052181365Floorbeam · corrodedAFT WET AREA FLOOR BEAM BS 947 LBL 52 SHOWS SIGNS OF CORROSION DOT L631<[01] REMOVED AND REPLACED CORRODED SECTION OF FLOOR BEAM AT STA. 947.5 LEFT SIDE IAW B737-800 SRM 53-70-51-2R-5-B00675.;[02] VERIFIED REMOVED AND REPLACED CORRODED SECTION OF FLOOR BEAM ATSDR SWAA2024052181366Floor Support · corrodedAFT WET AREA INTERCOSTAL AT BS 947 LBL 52 SHOWS SIGNS OF CORROSION DOT L639<[01] REMOVED AND REPLACED INTERCOSTAL PN 147A5660Y2 IAW B737-800 SRM 51-40-02 AND BAC DWG 147A5660;[02] VERIFIED REMOVED AND REPLACED INTERCOSTAL PN 147A5660Y2 IAW B737-800 SRM 51-40-0SDR SWAA2024052181367Web · corrodedAFT WET AREA AFT OF L2 DOOR AT 986 EVIDENCE OF CORROSION FOUND ON WEB STRUCTURE DOT L632<[01] REMOVED AND REPLACED WEB ASSY PN 147A5712U34 STA.986.5-1016 LBL 27.95-LBL43 IAW B737-800 SRM 51-40-02 AND BAC DWG 147A5700 REV- T05868-187 CAL DUE 16JUL24; T8356U CALSDR SWAA2024041574575Trim Motor · inoperativeELECTRONIC STABILIZER TRIM DID NOT WORK IN FLIGHT LANDED FLAPS 15; OVERWEIGHT BY 5100# NO HOT BRAKE ISSUES ELECTRONIC STABILIZER TRIM DID NOT WORK IN FLIGHT LANDED FLAPS 15 OVERWEIGHT BY 5100# NO HOT BRAKE ISSUES<[01] REMOVED AND REPLACED STAB TRIM MOTOR AS PESDR SWAA2024032868544Skin · delaminatedDURING WALK AROUND; FOUND DELAM AT R/H I/B AFT FLAP ON A PRIOR REPAIR DELAM ON EXISTING REPAIR AT R/H I/B AFT FLAP. 13 FROM I/B EDGE 3 FROM TRAILING EDGE. DELAM AREA 6 BY 6. SEE ATTACHED PIC FOR DETAILS.<[01] CW EA 24-157-00828SDR SWAA2024032768183Autothrottle Sys · unknownUNCOMMANDED THROTTLE REDUCTION ON CLIMBOUT AND AGAIN AT APPROX 2400FT AGL. NO RE-OCCURRENCE AFTER THAT<[01] COMPLIED WITH A/T BITE PROCEDURE IAW FIM TASK 22-31 (801). NO HISTORY OR CURRENT FAULTS NOTED AT THIS TIME. A/C OK FOR SERIVE.SDR SWAA2024013045986Skin · delaminatedRT INBOARD MAIN FLAP DELAMINATED AFT EDGE O/B OF FLAP AT WEDGE ASSY LOWER SKIN. RT INBOARD MAIN FLAP DELAMINATED AFT EDGE O/B OF FLAP<[01] REMOVED R/H INB FLAP WEDGE PER SRM 51-40-02;[02] REMOVED AND REPLACED RT. INBOARD MAIN FLAP AFT WEDGE ASSY. PER. AMM REF.SDR SWAA2024013045987Skin · delaminatedLT INBOARD MAIN FLAP DELAMINATED AT AFT EDGE O/B OF FLAP LOWER SKIN OF TRAILING EDGE WEDGE ASSY... LT INBOARD MAIN FLAP DELAMINATED AT AFT EDGE O/B OF FLAP<[01] REMOVED THE LEFT MAIN FLAP TRAILING EDGE WEDGE;[02] REMOVED AND REPLACED LT INBOARD MAIN FLAP AFT WSDR SWAA2023090597022Megaphone · inoperativeMEGAPHONE INOP<[01] R&R MEGAPHONE IAW AMM 25-64-00SDR SWAA2023090596978Megaphone · failedFLIGHT ATTENDANT MEGAPHONE WILL NOT TEST; NO BLINKING GREEN LIGHT<[01] RR BATTERIES IAW AMM 25-64-00SDR SWAA2023090596490Flashlight · failedAFT FLASHLIGHT RED LIGHT BLINKING AFT FLASHLIGHT REF LIGHT BLINKING<[01] REMOVED AND REPLACED FLASHLIGHT BATTERY ON AFT L/H INBD REF AMM 25-64-00SDR SWAA2023081790131Battery · dischargedBATTERY FOR L/H FWD ENTRY EMERGENCY EXIT LIGHTS REQUIRES REPLACEMENT DUE TO LOW CHARGE<[01] R/R BATTERY FOR FWD ENTRY EMERGENCY EXIT LIGHTS IAW AMM 33-51-06
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